This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Development of the Surface Thermal Environment for the Mars Scout Phoenix Mission
Technical Paper
2007-01-3239
ISSN: 0148-7191, e-ISSN: 2688-3627
Annotation ability available
Sector:
Language:
English
Abstract
Phoenix is NASA's first Mars Scouts Mission that will place a soft-lander on the Martian surface at a high northern latitude. Much of the Mars surface environmental flight data from landed missions pertains to the near-equatorial regions. However, orbital observations have yielded very useful data about the surface environment. These data along with a simple, but highly effective one-dimensional atmospheric model was used to develop the Phoenix surface thermal environment. As candidate landing sites were identified, parametric studies including statistical variations were conducted to prescribe minimum nighttime and maximum daytime temperature design Sols (a Martian day). Atmospheric effects such as clouds and ice were considered. Finally, recent candidate landing site imaging conducted by the Mars Reconnaissance Orbiter revealed that the prime site contained a much higher rock density than first thought. Candidate landing sites were reprioritized and thus the surface thermal environment required re-characterization. This paper will
summarize the evolution of the surface thermal environment and will describe the general system-level thermal design approach to contend with the landed environment.
Recommended Content
Authors
Citation
Tsuyuki, G., Tamppari, L., Martin, T., and Murphy, J., "Development of the Surface Thermal Environment for the Mars Scout Phoenix Mission," SAE Technical Paper 2007-01-3239, 2007, https://doi.org/10.4271/2007-01-3239.Also In
References
- Farguson C. “Mars Exploration Rover (MER) Project, Environmental Requirements Document, Revision E,” JPL Internal Document D-19272 25 July 2003
- Martin T. Z. Bridges N. Murphy J. R. “Modeling Near Surface Temperatures at Martian Landing Sites,” Journal of Geophysical Research-Planets, Paper Number doi: 10.1029/2003JE002063 2003
- Haberle R. M. Joshi M. Murphy J. R. Barnes J. B. Schofield J. T. Wilson G. Lopez-Valverde M. Hollingsworth J. L. Bridger A. F. C. Schaeffer J. “GCM Simulations of The Mars Pathfinder ASI/MET Data” Journal of Geophysical Research 104 8957 8974 1999
- Mellon M. Personal Communication 2004
- Mellon M. T. Jakosky B. Kieffer H. Christensen P. “High Resolution Thermal Inertia Mapping from The Mars Global Surveyor Thermal Emission Spectrometer” Icarus 148 437 455 2000
- Putzig N. E. Mellon M. T. Kretke K. A. Arvidson R. E. “Global Thermal Inertia and Surface Properties of Mars from The MGS Mapping Mission” Icarus 173 325 341 2005
- Natour M. “Phoenix Project, Environmental Requirements Document, Revision B,” JPL Internal Document D-27777 31 October 2006
- Ewell R. “Rover Solar Array Power FORTRAN Tool, pwrover-a” JPL Personal Communication 4 August 2002
- Vasvada A. “Phoenix GCM Run Request,” JPL Personal Communication 20 June 2006